M=3 Turbulent Boundary Layer Measurements at very High Reynolds Numbers.

Abstract

Experimental turbulent boundary layer measurements were made. Data was generated at supersonic speeds and very high Reynolds numbers to determine the effect of both unit and length Reynolds numbers on boundary layer profiles, thickness parameters, and skin friction measurements.

Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1977
Accession Number
ADA055952

Entities

People

  • Anthony W. Fiore

Organizations

  • Flight Dynamics Laboratory

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Fluid Mechanics
  • Friction
  • Layers
  • Measurement
  • Reynolds Number
  • Skin Friction
  • Thickness
  • Turbulent Boundary Layer

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow